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  1. 1
    Aerodynamic parameter estimation via fourier modulating function techniques

    Aerodynamic parameter estimation via fourier modulating function techniques by Pearson, A. E.

    Hampton, Va. : [Springfield, Va.] : National Aeronautics and Space Administration, Langley Research Center ; [National Technical Information Service, distributor], 1995
    Format: Government Document Book


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  2. 2
    Analysis of surface cracks at hole by a 3-D weight function method with stresses from finite element method

    Analysis of surface cracks at hole by a 3-D weight function method with stresses from finite element method

    Hampton, Va. : [Springfield, Va.] : National Aeronautics and Space Administration, Langley Research Center ; [National Technical Information Service, distributor], 1995
    Format: Government Document Book


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  3. 3
    Least squares finite element simulation of transonic flows

    Least squares finite element simulation of transonic flows by Chen, T. F.

    Hampton, Va. : [Springfield, Va.] : National Aeronautics and Space Administration, Langley Research Center ; [For sale by the National Technical Information Service], 1986
    Format: Government Document Book


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  4. 4
    The weight hierarchies and chain condition of a class of codes from varieties over finite fields

    The weight hierarchies and chain condition of a class of codes from varieties over finite fields by Wu, Xinwen

    [Washington, DC] : [Springfield, Va.] : [National Aeronautics and Space Administration] ; [National Technical Information Service, distributor], 1996
    Format: Government Document Book


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  5. 5
    Graphical interactive control design and implementation environment : final report for the period 1 May 1994 - 30 April 1996, contract no. NAS1-20201

    Graphical interactive control design and implementation environment : final report for the period 1 May 1994 - 30 April 1996, contract no. NAS1-20201 by Kosut, Robert L.

    [Washington, DC] : [Springfield, Va.] : [National Aeronautics and Space Administration] ; [National Technical Information Service, distributor], 1996
    Format: Government Document Book


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  6. 6
    Generalized INF-SUP condition for Chebyshev approximation of the Navier-Stokes equations

    Generalized INF-SUP condition for Chebyshev approximation of the Navier-Stokes equations by Bernardi, Christine

    Hampton, VA : [Springfield, Va.] : Institute for Computer Applications in Science and Engineering, NASA Langley Research Center ; [For sale by the National Technical Information Service], 1986
    Format: Government Document Book


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  7. 7
    Investigation of dispersion-relation-preserving scheme and spectral analysis methods for acoustic waves

    Investigation of dispersion-relation-preserving scheme and spectral analysis methods for acoustic waves by Vanel, Florence O.

    [Washington, D.C.] : [Springfield, Va.] : [National Aeronautics and Space Administration] ; [National Technical Information Service, distributor], 1995
    Format: Government Document Book


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  8. 8
    Analysis of corner cracks at hole by a 3-D weight function method with stresses from finite element method

    Analysis of corner cracks at hole by a 3-D weight function method with stresses from finite element method

    Hampton, Va. : [Springfield, Va.] : National Aeronautics and Space Administration, Langley Research Center ; [National Technical Information Service, distributor], 1995
    Format: Government Document Book


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  9. 9
    On adapted weighted polynomial preconditioning for Hermitian positive definite matrices

    On adapted weighted polynomial preconditioning for Hermitian positive definite matrices by Fischer, Bernd

    [Moffett Field, Calif.] : [Springfield, Va.] : Research Institute for Advanced Computer Science, NASA Ames Research Center ; [National Technical Information Service, distributor], 1992
    Format: Government Document Book


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  10. 10
    Statistically generated weighted curve fit of residual functions for modal analysis of structures

    Statistically generated weighted curve fit of residual functions for modal analysis of structures by Bookout, P.S

    Marshall Space Flight Center, Ala. : [Springfield, Va.] : National Aeronautics and Space Administration, George C. Marshall Space Flight Center ; [National Technical Information Service, distributor], 1995
    Format: Government Document Book


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  11. 11
    Analysis of modified SMI method for adaptive array weight control

    Analysis of modified SMI method for adaptive array weight control by Dilsavor, Ronald Louis

    [Washington, DC] : [Springfield, Va.] : [National Aeronautics and Space Administration] ; [National Technical Information Service, distributor], 1989
    Format: Government Document Book


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